Electronic fuel injector control for rotary vacuum fuel conversion device

ABSTRACT

An electronic fuel injector control is provided for selectively activating fuel injectors for introducing macroscopic liquid fuel droplets into the vacuum chamber of a device for converting fuel into microscopic fuel droplets and fuel vapor. The control has a rotatably mounted rotor shaft, connectable to the rotor in the vacuum chamber and fuel conversion signal device to provide first periodic signal pulses responsive to the angular rotational position of the rotor shaft. Engine sensor electronics is responsive to input signals from engine sensors indicative of engine condition and is further responsive to an output signal pulse from the fuel conversion signal device each time the vane sweeps past the fuel injector. A sensor is provided which is responsive to the desired angular position of the engine crankshaft to provide second periodic signal pulses. An electric motor connected to the rotor shaft, when running, provides a blocking signal to the engine sensor electronics to block the signal pulses from the fuel conversion signal device so that the fuel injectors are activated only in response to the crankshaft pulses.

TECHNICAL FIELD

This is a continuation-in-part application of copending U.S. Ser. No. 958,006, filed Oct. 8, 1992, now U.S. Pat. No. 5,226,400 and entitled "Device For Conversion of Liquid Fuel Into Fuel Vapor and Microscopic Liquid Droplets".

This invention relates to a device for converting liquid fuel into fuel vapor and microscopic liquid fuel particles prior to introduction into an intake manifold of an internal combustion engine. More particularly, the invention relates to the injection of macroscopic liquid fuel droplets into a rotary vane vacuum chamber wherein some of the macroscopic liquid fuel droplets are converted to a gaseous fuel and the rest are converted to microscopic liquid fuel droplets. After discharge from the vacuum chamber the gaseous fuel and microscopic liquid fuel droplets are mixed with air and supplied to the intake manifold of the internal combustion engine. An electronic control is provided for causing fuel injectors to inject the macroscopic liquid fuel droplets into the vacuum chamber at an appropriate time in its cycle and in relation to the position of the engine crankshaft.

BACKGROUND ART

It is well understood that the greater the vaporization or gasification of liquid fuel that can be accomplished the greater the surface area of the fuel which is subject to oxidation and therefore the higher the rate of combustion. Many individuals working in the field felt that if complete conversion of the fuel to the gaseous state could be accomplished, a highly efficient clean operating engine could be provided. Attempts to completely gasify liquid hydrocarbon fuel go back many years. However, all of these attempts have had significant shortcomings. In some instances, the devices did not completely vaporize the fuel and therefore the expected increase in efficiency did not materialize. In other cases, the devices were of such a complex nature as to negate any real benefit from them or require such high power inputs themselves that even though a greater fuel efficiency was realized, the increased power needs negated this benefit. The complete conversion of fuel to vapor created another unexpected problem. Although the fuel would rapidly and completely burn, it was discovered that the expansion of the fuel in forming a gas occurred too early. Therefore, the density of the fuel, when mixed with air was so low that not enough fuel could be directed into the combustion chambers of the engine to generate power equal to other state of the art devices such as carburetors, throttle body injection systems or direct port injection systems.

One of the most noted prior art devices which was developed by Charles Nelson Pogue in the 1930s was a carburetor for the vaporization of gasoline which has been widely advertised as the "two hundred mile per gallon carburetor". This device has never enjoyed wide commercial success because it is nearly as large and cumbersome as the engine it is meant to fuel and it requires an operating temperature which approaches the flash point of the fuel, such as gasoline, so that the potential for an explosion is quite great.

A device for vaporizing fuel, such as diesel fuel is disclosed in U.S. Pat. No. 1,806,581 to Bethenod for "Fuel Supply System For Internal Combustion Engines of Variable Load For Using Heavy Fuels". The diesel fuel is supplied through a conventional gasoline carburetor and air is drawn through an intake by means of a vacuum pump. This system is an open system, i.e., air in large quantities is continuously drawn in from the atmosphere by a first vacuum pump. A second vacuum pump is intended to pull a vacuum on the air-fuel mixture in a reservoir to vaporize the fuel whereupon it is fed into a manifold of an engine which is supplied with still an additional air intake. Heat exchange means are provided around the reservoir and again near the intake manifold to minimize fluctuations in fuel temperature. Because the system is open, large quantities of air are drawn through it making it very difficult to draw a sufficient vacuum to substantially vaporize any fuel which is not vaporized directly by the carburetor. In other words, for such a device to operate effectively it would be necessary to provide such a huge vacuum pump that the fuel savings, if any, would be negligible. Alternatively, with a smaller vacuum pump the fuel is not properly vaporized in an open system because atmospheric air is constantly being drawn into the system.

Another device for providing gaseous fuel to the carburetor of an internal combustion engine is shown in U.S. Pat. No. 3,630,698 to Joseph H. Baldwin for "Fuel System". In this device, gaseous vapors are drawn from a vacuum chamber by means of a manifold vacuum. The vacuum chamber contains a supply of liquid fuel which is replenished through a float valve. Two potential problems are associated with this type of device. First, the vacuum from the manifold may not be sufficient under certain load conditions to provide sufficient fuel to the engine. Second, by drawing the gaseous vapors off of a body of liquid gasoline the lighter hydrocarbons are boiled off first, leaving a relatively heavy liquid hydrocarbon, frequently referred to as "strip oil". Therefore, in order to keep them working properly, means must be provided to regularly withdraw the strip oil and replace it with fresh gasoline.

Another device for vaporizing gasoline is disclosed in Rose, et al. U.S. Pat. No. 4,040,403 for "Air Fuel Mixture Control System". In this device, fuel is supplied to a vaporizer wherein the level of the liquid fuel in the vaporizer is controlled by a float valve. Hot exhaust gases from the engine are boiled through the liquid gasoline causing a portion of it to be vaporized and carried to the engine. The device includes a complex amplifying system for adjusting the air-fuel mixture and a separator for taking out any fuel droplets from the fuel as it is vaporized in the vaporizer. With this device, the lighter hydrocarbons will be vaporized leaving behind the heavier hydrcarbons or strip oil.

Johnson U.S. Pat. No. 4,175,525 for "Fuel Vaporizer System For Internal Combustion Engines" discloses a sealed vaporization system connected between a fuel supply line and the intake manifold of an internal combustion engine and operated in parallel with a carburetor. A float valve is provided in this device to control the flow of liquid fuel to a chamber wherein it is vaporized and fed to a carburetor. The lighter hydrocarbons will be boiled off the liquid fuel before the heavier hydrocarbons, leaving strip oil in the chamber.

Additional devices for vaporizing fuel are disclosed in James E. Gilmor U.S. Pat. No. 4,483,305 for "Fuel Vaporization Device" and James E. Gilmor U.S. Pat. No. 4,483,307 for "Fuel Vaporization Device For Internal Combustion Engine". These devices are designed to instantaneously vaporize all of the fuel.

Meier et al. U.S. Pat. No. 4,522,183 for "Method For Converting a Retrograde Substance to the Gaseous State" is directed to a method wherein the fuel is prepressurized and heated and the pressure released for abruptly converting a retrograde fuel to a gaseous state. While the method may be effective to accomplish its intended result, it is not believed that sufficient fuel can be provided to an internal combustion engine by the practice of this method to operate it satisfactorily, particularly under load.

The ultimate carburetion system would be one in which a small percentage of the fuel is vaporized and the rest of the fuel is converted to microscopic liquid fuel droplets prior to introducing the fuel into the intake manifold of an internal combustion engine. When mixed with air in the manifold the vaporized fuel and the microscopic fuel droplets disperse with some additional vaporization.

For convenience, gaseous fuel will be referred to as "vapor" or "vaporized fuel"; liquid fuel droplets of a size not visible with the naked eye, under normal lighting conditions, will be referred to as "microscopic" particles or droplets and liquid fuel droplets of a size which is visible with the naked eye will be referred to as "macroscopic" droplets. Ideally, macroscopic liquid fuel droplets from a suitable source, such as one or more fuel injectors, are converted to a mixture consisting of a small percentage of fuel vapor and a large percentage of microscopic fuel droplets. This mixture will be referred to as "converted fuel".

DISCLOSURE OF THE INVENTION

In accordance with the present invention, a device for converting a combustible liquid fuel into converted fuel having a smaller proportion of vapor and a larger proportion of microscopic fuel droplets, mixing the converted fuel with air in a manifold to convert more of the converted fuel to a vapor and transferring the converted fuel and air mixture into a combustion chamber is provided. The device includes a vacuum chamber formed as a cylindrical housing wall having a longitudinal axis with at least one fuel inlet in the housing wall and a fuel outlet in the housing wall offset from the inlet. An eccentrically mounted cylindrical rotor is provided within the housing wall for rotation about a longitudinal axis about bearings mounted in opposite end walls. The rotor has a plurality of radial slots and a generally rectangular vane slidably received in each of the slots. The vanes are urged outwardly against the housing wall when the rotor is rotated.

For lubrication the inner surface of the housing may be coated with a lubricous material. This may be a polytetrafluoroethylene (PTFE) matrix such as Teflon®. Alternatively a sleeve may be used inside of the housing which is made of a polyamid, such as Torlon®. The vanes are made of a polyamide having a durometer or hardness which is less than that of the lining. If desired, spring means can be provided for urging the vanes outwardly against the housing wall. The vanes are arranged in opposing relationship and the spring means can include a pin positioned between opposite springs to urge the vanes against the housing wall.

More particularly, the rotor has a surface which comes into near contact, e.g., within two-thousandth of an inch, with the cylindrical wall along a near contact line lying in a common plane with the axis of the rotor to form a vacuum chamber between the rotor and the cylindrical wall. A liquid fuel inlet in the form of a fuel injector can be mounted through each end wall in opposing relationship with each other. The injectors are angularly spaced within the vacuum chamber to the upstream side of the plane and as close to the near contact line as the introduction of fuel through the injectors will permit. Alternatively, the injectors can be mounted in the cylindrical wall of the housing in the same angular relationship. The converted fuel outlet extends through the cylindrical wall of the vacuum chamber into communication with an air-fuel mixing chamber just upstream of the near contact line.

The fuel injectors inject macroscopic droplets of liquid fuel through the inlets into the vacuum chamber where it is converted to microscopic fuel and vaporized fuel. This is accomplished by a combination of vacuum, expanding absorbed gases and water vapor in the macroscopic fuel droplets, and mechanical and heat energy from the action of the vacuum pump.

An air plenum has an air-fuel mixing chamber connected to the vacuum pump outlet port for receiving and mixing the converted fuel with air introduced through an air inlet port in the air plenum. An air intake passageway connects at one end of the mixing chamber to the air inlet port and is at substantially right angles to the converted fuel outlet from the vacuum chamber. An air-fuel discharge passageway is provided on the opposite side of the intake passageway for supplying the mixture of air and converted fuel to the manifold and then to the engine for combustion. The mixing chamber is larger in area than the intake passageway so that the air slows down as it passes through the mixing chamber creating a tumbling effect to allow for thorough mixing with the converted fuel. In addition, a diverter is provided in the center of the mixing chamber to further create turbulent flow of the air to assure thorough mixing.

Additionally, an electronic fuel injector control is provided for selectively activating the fuel injectors for introducing macroscopic liquid fuel droplets into the vacuum chamber of the fuel conversion device. The control has a rotatably mounted rotor shaft connectable to the rotor in the vacuum chamber, and fuel conversion device signal means to provide first periodic signal pulses responsive to the angular rotational position of the rotor shaft. Engine sensor electronics is responsive to input signals from engine sensors indicative of engine condition and is further responsive to the output signal pulses from the fuel conversion device signal means. A signal pulse is provided each time a vane sweeps past the fuel injector. A sensor is provided which is responsive to the desired angular position of the engine crankshaft to provide second periodic signal pulses. An electric motor connected to the rotor shaft, when running, provides a blocking signal to the engine sensor electronics to block the first signal pulses from the fuel conversion device signal means so that the fuel injectors are activated only in response to the crankshaft pulses. The signal device for the fuel conversion device signal means can be an optical sensing device wherein a disk is mounted for rotation on the rotor shaft and has a pair of apertures adjacent its periphery spaced 180° apart and a light beam is directed toward the peripheral edge of the disk for transmission of a light beam through the apertures to activate a light switch in response to the correct position of the vanes within the vacuum chamber.

From the foregoing, the advantages of this invention are readily apparent. A very simple, and therefore economical, device has been provided for converting microscopic liquid fuel particles into converted fuel having the proper ratio of vaporized fuel and microscopic fuel particles. By use of vacuum, expanding absorbed gases, mechanical energy and thermal energy the converted fuel is formed. The converted fuel is mixed with air in a novel mixing chamber which causes-thorough mixing with some additional evaporization and droplet breakup. Thus, the combustion of the fuel in the engine will be enhanced, thereby minimizing the amount of unburned hydrocarbons and maximizing fuel economy. By utilizing a lubricous material, the problems of lubricating the parts in a fuel-rich vacuum environment, wherein the lubricant would be dissolved and may vaporize, is minimized. Also the fuel injectors can be activated at the most advantageous time during the cycle of the fuel conversion device.

Additional advantages will become apparent from the description which follows, taken in conjunction with the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a fragmentary perspective view of a vehicle having the fuel conversion device of this invention installed therein;

FIG. 2 is an enlarged side elevation of the fuel conversion device of this invention connected to the intake manifold of an internal combustion engine;

FIG. 3 is an enlarged horizontal section, taken along line 3--3 of FIG. 2, showing the fuel converter of this invention and associated drive mechanism therefor;

FIG. 4 is a horizontal section, taken along line 4--4 of FIG. 3, showing details of a one-way clutch and bearing mounts for the fuel converter;

FIG. 5 is an enlarged horizontal section, taken along line 5--5 of FIG. 4, showing details of the air-fuel mixing chamber and rotor;

FIG. 6 is a horizontal section, taken along line 6--6 of FIG. 5, showing additional details of the mixing chamber and rotor;

FIG. 7 is a vertical section, taken along line 7--7 of FIG. 5, showing further details of the mixing chamber;

FIG. 8 is an exploded view of the rotor showing the vanes and associated parts;

FIG. 9 is a diagrammatical view of the fuel converter of this invention connected to an internal combustion engine, showing typical electronic sensing devices to control the fuel converter;

FIG. 10 is a fragmentary enlarged vertical section, similar to FIG. 5, but showing the vane in the desired position for fuel injection;

FIG. 11 is a diagrammatic perspective view of the fuel converting device of this invention showing the electronic fuel injector control; and

FIG. 12 is an enlarged fragmentary section, taken along line 12--12 of FIG. 11 showing details of the optical sensor.

BEST MODE FOR CARRYING OUT THE INVENTION

As illustrated in FIG. 1, the fuel converter 10 of this invention is installed in a vehicle 12 adjacent the engine 14. The fuel converter includes a generally cylindrical housing 16 having a longitudinal axis A and opposed front end plate 18 and rear end plate 20, as shown in FIG. 4, to form a vacuum chamber 22. Suitable lubrication within the vacuum chamber is a problem. Liquid lubricants, i.e., oils and greases, will not work because they will be dissolved and removed by the fuel and will tend to evaporate, particularly when gasoline is used as a fuel because of the higher temperatures. To overcome this, the housing has a lining 17 made from a lubricous material, such as a polyamide. One such polyamide which is suitable is Torlon®. Alternatively, a PTFE coating, such as a Teflon® matrix can be used. Fuel is supplied by means of a fuel pump 24 through a fuel line 26 to fuel atomizing devices, such as fuel injectors 28. A fuel pressure regulator 30 is located in return fuel line 32 for returning fuel which is not used by the fuel injectors to the fuel tank (not shown).

Rotor 34, shown in FIG. 4, is journaled in a front bearing 36 mounted in front end plate 18 and a rear bearing 38 mounted in rear end plate 20. The rotor is mounted for rotation about a longitudinal axis A spaced laterally from housing axis B, as best seen in FIGS. 4 and 5. The rotor makes near contact with the housing wall 16 along line C. In one form of the invention, the spacing along line C is approximately one-thousandth of an inch. Conveniently, the heat generated by these bearings during operation of the fuel converter 10 will heat the end plates and the respective injectors 28 to preheat the fuel before it passes into vacuum chamber 22. Also, heating coils 40 can be provided around each fuel injector 28 to pre-heat the fuel for cold starts when the ambient temperature is extremely low. Alternatively, heating coils (not shown) could be provided in the walls or ends of vacuum chamber 22 to reheat the fuel. The injectors 28 lie on the upstream side of a plane D formed by axis A and line C and as near to line C as is possible and still inject the fuel. The reason for this is so the fuel remains in the vacuum chamber as long as possible to more greatly facilitate the formation of converted fuel.

The rotor 34 is connected by coupling 42 to a driven shaft 44. The forward end of driven shaft 44 is connected through a one-way slip clutch 46 to a drive shaft 48. This drive shaft is supported in bearing 50 at the forward end of cylindrical housing 52. The other end of housing 52 is provided with a flange 54 attached to front end plate, as by bolts 56 spaced around the periphery thereof. Drive shaft 48 is driven by pulley 58 which in turn is driven by belt 60 driven from pulley 62 attached to pully shaft 64 of engine 14, as best seen in FIG. 2.

During cold weather, the starter motor of the vehicle may not turn the engine and the fuel converter 10 at sufficient speed to create sufficient vacuum to convert the fuel from macroscopic liquid droplets to vapor and microscopic liquid particles at a sufficient rate to start the engine. Therefore, if required, an electric motor 66 can be mounted behind the fuel converter 10 which will be operated directly off the battery (not shown) to drive the rotor through a stub shaft 68 connected thereto at a much higher speed so that enough fuel will be converted and supplied to the engine to start it. This is possible because one-way clutch 46 allows driven shaft 44 and rotor 34 to turn faster than drive shaft 48. By way of example, electric motor 66 may rotate rotor 34 at 750 rpm or more while the engine is turning at 150 rpm during starting. After starting, electric motor 66 will be turned off and the engine and rotor will rotate at the same speed.

After conversion, the fuel passes from vacuum chamber 22 into a plenum 70 where it is mixed with air supplied through conduit 72 so that the air flow is at right angles to the converted fuel to assure maximum mixing as more fully described below. Conveniently, the air is drawn through-a filter 74, connected to the other end of conduit 72.

Turning now to FIGS. 5-9, the rotor 34 has a plurality of vanes, such as two opposed vanes 76 which are urged apart as by a pair of leaf springs 78 received in recesses 80 of the vanes. A pin 82 has opposite ends bearing against leaf springs 78 and reciprocated within passageway 84 extending through rotor 34 between vanes 76. The vanes are coated with the same lubricous material as the housing liner, but having a lesser hardness or durometer than the housing liner. This assures that most of the wear that occurs will be along the edge of the vanes, which can be easily replaced. As can be seen, with rotor 34 mounted for rotation eccentrically with respect to housing 16, the vanes will be urged against the inner surface of the housing but will move reciprocally back and forth as the rotor rotates. Since the spacing of the two vanes remains substantially constant, there will be little flexure of springs 78 and therefore the chance of failure of the springs through extended use is very minimal. In fact, when the pump is in operation centrifugal force will hold the vanes outwardly. However, for starting purposes it is desirable to have the springs in place to keep the vanes extended. With the use of starter motor 66, for most applications springs 78 and pin 82 will not be needed since the centrifugal force on the vanes created when motor 66 is energized will be sufficient.

The fuel injected into vacuum chamber 22 as macroscopic liquid fuel droplets is converted to vapor and microscopic fuel particles which are moved around the chamber by the vanes and discharged through a pair of outlet ports 86, located downstream of plane D.

As best understood at the present time, a number of forces act upon the macroscopic liquid fuel droplets introduced by the fuel injectors. These are:

1. Vacuum, which is a direct result of the vacuum environment of the device, causes rapid vaporization of fuel from the surface of the droplets thereby causing some reduction in the sizes of all droplets.

2. Absorbed gas expansion, which also is a direct result of the vacuum environment of the device, caused absorbed gases such as nitrogen, oxygen, water vapor and other atmospheric gases to expand within the macroscopic droplets blowing them apart into smaller microscopic droplets thereby exposing more surface area for further boiling off of liquid fuel from the microscopic droplets. Evaporization alone is not sufficient to cause both significant vaporization and droplet size reduction, particularly with less volatile fuels such as alcohols and alcohol mixtures. The vaporization is a self-limiting process because the evaporation process absorbs heat from the droplets which rapidly reduces their temperatures such that the evaporation rate rapidly decreases to an insignificant level. The absorbed atmospheric gases and most volatile species of the fuel rapidly expand causing eruptive boiling of the droplets breaking them into much smaller droplets.

3. Mechanical energy from vanes, rotor and housing agitate the macroscopic liquid droplets to distort and spread them out and break the surface tension within the droplets to further release absorbed gases.

4. Heat energy from contact with vanes, rotor and housing raises the temperature of liquid droplets to enhance vaporization and expansion and release of absorbed gases.

The foregoing explanation is believed to be accurate, to the extent that the forces acting upon the fuel droplets are understood at the present time. However, it should be understood that there may be additional forces acting on the droplets and/or the magnitude of the effect of the forces described above may be greater or lesser than presently understood.

Turning to FIG. 7, air flows through conduit 72 past a butterfly valve 88 controlled through a butterfly linkage 90 connected to the accelerator (not shown). This intake air passes through a throat 92 in plenum 70 and into a larger mixing chamber 94 which includes outlet ports 86 from vacuum chamber 22 and also a center dividing wall 96 between outlet ports 86 and curved wall 97 opposite ports 86. Thus, as the air-moves from throat 92 into larger chamber 94, its flow will slow down. The dividing wall 96 and curved wall 97 cause turbulence in the air so that it mixes thoroughly with the gaseous fuel and microscopic fuel particles being discharged into chamber 94 from discharge openings 86 which are at right angles to the flow of air through chamber 94. The relatively warm air which is mixed with the fuel will heat the microscopic fuel droplets causing additional evaporation and droplet size reduction. By injecting the converted fuel into the air at right angles, good mixing of the air and fuel is assured which will improve the burning of the fuel in the cylinders of the engine. Thus, a very efficient and clean burn is assured.

As best seen in FIG. 9, an electronic fuel management (EFM) control module 104 is provided. This control module receives various signals from RPM sensor 106 mounted on engine 14 through a wire 108. A temperature sensor 110 on engine 14 provides a signal through wire 112 to the control module. The control module processes these signals and provides a signal through wire 114 to fuel injectors 28, which provides fuel to the converter in accordance with the parameters sensed by the control module. Thus, if butterfly valve 88 is opened to provide more air to the engine, the manifold pressure sensor 116 will provide a signal to control module 104 which will cause the control module to send a signal through wire 114 to the fuel injectors to open them further to provide more fuel to pump 10. When the butterfly valve 88 is closed due to releasing the accelerator, the reverse will occur. The temperature sensor 110 is provided for cold starts. It is useful for engines fueled by alcohol and provides further input to the control module for regulating the fuel injection when the engine is initially started. A suitable system has been found, an engine management system manufactured by Digital Fuel Injection Incorporated at 37732 Hills Tech Drive, Farmington Hills, Mich. 48331, which has external program capabilities to adjust fuel ratio across the entire range, for various fuels. Also, most original equipment automobile manufacturers' management systems can be modified to manage the fuel converter of this invention.

Additionally, a manifold vacuum sensor 116 is connected to control module through wire 118 and an oxygen sensor 120 on engine tailpipe 122 is connected by wire 124 to control module 104. Many other sensors (not shown) may be provided to measure other engine conditions or functions for electronic fuel management.

As of the date of this application, applicant's fuel conversion device has only been operated at an elevation of approximately five-thousand feet above sea level. Thus, the parameters set forth below are for this elevation and would vary at either higher or lower elevations in accordance with well-known physical laws. In a fuel conversion device wherein the vacuum chamber 22 is formed within housing 16 which has an interior diameter of 2.60 inches and a length of 3.00 inches and the diameter of rotor 34 is 2.50 inches. When the rotor is rotating at an idle speed of between 700 and 750 rpm, the device draws approximately 24.5 inches of mercury at an ambient temperature of 80° F. before introduction of fuel. At operating speeds between 1700 and 2000 rpm, after fuel is introduced in sufficient quantity to operate the engine at these speeds, the device stabilized at 23.5 to 23.7 inches of mercury. At these speeds and at ambient temperatures of between 45° F. and 80° F., the device will produce at the outlet converted fuel, a smaller portion of which is vapor, and a larger portion of which is microscopic liquid droplets. As the microscopic fuel droplets move through the vacuum chamber, the mixing chamber and the manifold, additional microscopic fuel droplets are vaporized as previously described.

By way of example, vacuum chamber 22, of the size described above, is connected to mixing chamber 94, wherein throat 92 has a diameter of 1.50 inches and an outlet into the manifold of 1.90 inches. The outlet ports 86 which communicate the vacuum chamber with the mixing chamber each are 1.0625 inches wide by 1,375 inches high. The dividing wall 96 is 1.9375 inches long and 0.50 inches wide.

The invention has been described as utilizing a single vacuum pump with an engine. However, it is contemplated that a very small vacuum pump could be used to supply fuel to each cylinder to the engine for some applications.

It is important for the most efficient operation of the fuel converter 10 that fuel injectors 28 be activated at an appropriate time during the rotation of rotor 34 and its associated vanes 76. This appropriate time is just after the trailing edge of one of the vanes 76 has swept past fuel injectors 28, such as the position shown in FIG. 10. At this point in the rotation of rotor 34, the fuel will be introduced into an intake area 100 just before converted fuel is discharged from discharge area 102 which is the area bounded by the leading edge of that same vane and the trailing edge of the opposite vane. By injecting the fuel at that this point, the physical time that the fuel is in fuel converter 10 is maximized so that as much fuel as possible can be converted from macroscopic fuel droplets to microscopic fuel droplets and fuel vapor in accordance with the process described above. This becomes more and more important with increased engine and fuel converter speed because the greater the RPM of the fuel converter 10, the shorter the time duration for the fuel to be present in fuel converter 10 to be converted during each rotation.

As shown in FIG. 11, electric motor 66 is connected to the rotor by means of a rotor shaft 104. Intermediate the ends of shaft 104 is a disk 106 having a pair of apertures 107 and 108 adjacent the periphery thereof and spaced 180° apart. Disk 106 is fixedly attached to shaft 104 and is oriented so that apertures 107 and 108 are aligned with the position of vanes 76 within fuel converter 10. An optical switch device 110 is provided which encircles one edge of the disk so that when an aperture is aligned therewith, the device projects a light beam by means of light 109 through the aperture to enable an optical switch 110 to provide an electrical output pulse. Although an optical switch device 110 has been illustrated, it will be understood that the same objective could be accomplished by use of magnetic elements on the disks spaced 180° apart which are sensed by a magnetic sensing device adjacent the disk. Also, devices that utilize the Hall Effect or mechanical devices could be used as well as one skilled in the sensing art will recognize.

The engine crankshaft 112 has magnetic coding or other indicia 114 thereon which provides a signal during each revolution to sensor 116 which provides a crankshaft output pulse signal each time the crankshaft is in the correct rotational position whereby the engine cylinders are properly located for accepting fuel. Conveniently, sensor 116 is one of many engine sensors 118 that provide signal inputs to the engine electronics 120 which in turn provides an appropriate output signal to the fuel injectors 28.

With conventional fuels, such as gasoline, electric motor 66 may not be necessary. However, for cold starts with alternative fuels, such as ethanol and methanol, it may be necessary to spin the fuel converter 10 by means of motor 66 at high RPMs, such as 3500 RPMs, compared to the 300 to 500 RPMs of the engine obtained from the engine starter motor (not shown). This is required in order to get enough fuel to the engine for initial ignition under cold start conditions. Under such conditions when the starter button (not shown) for the engine is depressed the starter motor and the electric motor will be energized simultaneously. During the operation of electric motor 66 a steady signal will be provided to AND gate 122 and to an invertor 124. Thus, every time there is a crankshaft output pulse signal from sensor 116, AND gate 122 will be activated to provide a signal to diode 126 which is fed through amplifier 128 to the engine electronics 120. Every time there is a pulse from sensor 116, engine electronics 120 will fire or activate fuel injectors 28. Since there will be no signal from invertor 124 to AND gate 130 the output pulse signal from optical switch 110 is inhibited by AND gate 130.

Once the engine has started, electric motor 66 will stop running and the output signal from it will cease. This will inhibit AND gate 122 but now invertor 124 will provide a signal to AND gate 130 which will provide an output signal every time there is a pulse from optical switch 110. This output signal will activate diode 132 which will provide a signal through amplifier 128 to engine electronics 120. Thus, the output from engine electronics 120 for firing injectors 28 will occur each time there is a signal from optical switch 110 indicating that the rotor 34 and associated vane 76 are in the position shown in FIG. 10. Under normal operating conditions, the fuel will be injected into fuel converter 10 as early in its cycle as possible to allow maximum time for the fuel conversion to take place before fuel is discharged through discharge opening 86.

From the foregoing, the advantages of this invention are readily apparent. A fuel converter has been provided in the form of a vacuum pump into which liquid fuel is injected in the form of macroscopic liquid particles in metered quantities into a vacuum chamber. The internal components of the vacuum chamber are made of or coated with a lubricous material. A portion of the fuel is vaporized into gaseous fuel and the rest is converted into microscopic liquid particles. This fuel is moved from the inlet to the outlet ports by sweeping vanes. After passing through the outlets, the fuel is mixed with air in a plenum wherein the fuel enters a plenum at substantially right angles to the direction of the fuel to assure thorough mixing. The plenum opens from a narrower throat into a larger mixing chamber which contains a dividing wall. This causes the air and fuel to mix thoroughly before it is introduced into the manifold and engine. By use of vacuum, expanding absorbed gases, mechanical energy and thermal energy the converted fuel is formed. The converted fuel is mixed with air in a novel mixing chamber which causes evaporation and expansion of additional fuel droplets. The entire system is operated by an electronic fuel management control module which receives numerous signals to provide information which is assimilated in the control module and provides an output signal to the fuel metering device to control the amount of fuel introduced into the pump.

This invention has been described in detail with reference to a particular embodiment thereof, but it will be understood that various other modifications can be effected within the spirit and scope of this invention. 

We claim:
 1. An electronic fuel injector control for selectively activating fuel injector means for introducing macroscopic liquid fuel droplets by means of fuel injectors into a cylindrical housing of a vacuum chamber of a fuel conversion device for converting the macroscopic droplets into converted fuel in the form of a mixture of microscopic liquid droplets and vaporized fuel for discharge from the vacuum chamber into the cylinders of an engine, said vacuum chamber containing a rotor, said fuel injector means controlled in response to the rotational position of vanes on the rotor relative to the location of the fuel injectors in the vacuum chamber, said control comprising:a rotatably mounted rotor shaft connectable to the rotor for rotating the rotor within the cylindrical housing; signal enabling means on said rotor shaft providing first periodic signal pulses responsive to the angular rotational position of said rotor shaft; and engine sensor electronics responsive to input signals from engine sensors indicative of engine conditions, and further responsive to each first output signal pulse from said signal enabling means to provide an output signal to activate the fuel injectors to provide a metered quantity of macroscopic fuel droplets to the vacuum chamber.
 2. Apparatus, as claimed in claim 1, wherein:said signal enabling means provides said first signal pulses each time one of the vanes sweeps past the fuel injector.
 3. Apparatus, as claimed in claim 1, further including:a sensor responsive to a desired angular position of the engine crankshaft, which indicates that the engine cylinders are in optimum position for receiving a fuel charge, providing second periodic signal pulses, said sensor being one of the engine sensors; and an electric motor connected to said rotor shaft for optional use during engine start-up, said motor providing a blocking signal, when said motor is running, to said engine sensor electronics to block said first signal pulses so that the fuel injectors are activated only in response to said second periodic signal pulses.
 4. Apparatus, as claimed in claim 1, wherein said signal enabling means includes:a disk mounted for rotation with said rotor shaft, said disk having a pair of spaced signal facilitating means adjacent the periphery of said disk spaced 180° apart; and sensing means mounted adjacent said periphery of said disk for producing said first periodic signal pulse each time said signal facilitating means passes said sensing means.
 5. Apparatus, as claimed in claim 1, wherein said signal enabling means includes:optical sensing means.
 6. Apparatus, as claimed in claim 5, wherein said optical sensing means includes:a disk mounted for rotation with said rotor shaft, said disk having a pair of apertures adjacent the periphery of said disk spaced 180° apart; light beam producing means mounted adjacent one side of said periphery of said disk for directing a beam of light through said apertures each time they become aligned with said light producing means; and a light switch mounted on the opposite side of said periphery of said disk for producing said first periodic signal pulse each time the light beam passes through said aperture.
 7. A method of activating fuel injectors in a cylindrical vacuum chamber of a fuel conversion device, for converting macroscopic fuel droplets into converted fuel in the form of microscopic fuel droplets and vaporized fuel to be supplied to an engine, in timed relationship to the rotational position of vanes on a rotor in the vacuum chamber and the rotational position of the crankshaft of the engine, said method comprising the steps of:sensing the rotational position of the vanes; sensing the rotational position of the crankshaft; and activating the fuel injectors when both the vanes and the crankshaft are in a desired position.
 8. A method of activating fuel injectors in a cylindrical vacuum chamber of a fuel conversion device, for converting macroscopic fuel droplets into converted fuel in the form of microscopic fuel droplets and vaporized fuel to be supplied to an engine, in timed relationship to the rotational position of vanes on a rotor in the cylindrical vacuum chamber and the rotational position of the crankshaft of the engine, said method comprising the steps of:sensing the rotational position of the vanes; sensing the rotational position of the crankshaft; activating an electric motor during start-up; providing a blocking signal in response to activation of the electric motor to inhibit the sensing of the rotational position of the vanes; and activating the fuel injectors only in response to the rotational position of the crankshaft. 